LEADER 00803nam0-22002891i-450- 001 990003988070403321 005 20060912143417.0 035 $a000398807 035 $aFED01000398807 035 $a(Aleph)000398807FED01 035 $a000398807 100 $a20031217d1971----km-y0itay50------ba 101 0 $aeng 102 $aGB 200 1 $aIntroduction to marine chemistry$fJohn Price Riley, Roy Chester 210 $aLondon$cAcademic Press$d1971 300 $aBibl. Ing. Sanitaria 610 0 $aScarichi a mare 700 1$aRiley,$bJohn Price$0295110 701 1$aChester,$bRoy$0295111 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990003988070403321 952 $a15 G/3-11$fDINID 959 $aDINID 996 $aIntroduction to marine chemistry$9473994 997 $aUNINA LEADER 01971oam 2200565 450 001 9910717162103321 005 20220210090328.0 035 $a(CKB)5470000002528594 035 $a(OCoLC)1156323793 035 $a(EXLCZ)995470000002528594 100 $a20200602d1939 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aWind-tunnel investigation of an N.A.C.A. 23021 airfoil with two arrangements of a 40-percent-chord slotted flap /$fby Frank Duschik 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939. 215 $a1 online resource (11 pages, 11 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 728 300 $a"September 1939." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 10). 606 $aAerofoils 606 $aSlotted flaps (Airplanes) 606 $aWind tunnel testing 606 $aAerodynamics 606 $aAerodynamics$2fast 606 $aAerofoils$2fast 606 $aSlotted flaps (Airplanes)$2fast 606 $aWind tunnel testing$2fast 615 0$aAerofoils. 615 0$aSlotted flaps (Airplanes) 615 0$aWind tunnel testing. 615 0$aAerodynamics. 615 7$aAerodynamics. 615 7$aAerofoils. 615 7$aSlotted flaps (Airplanes) 615 7$aWind tunnel testing. 700 $aDuschik$b Frank$01393030 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910717162103321 996 $aWind-tunnel investigation of an N.A.C.A. 23021 airfoil with two arrangements of a 40-percent-chord slotted flap$93448628 997 $aUNINA